N563AA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
40 reports on file, 1995-10-02 – 2010-11-04.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,208 hrs · 33,427 cycles
CEILING EMERGENCY LIGHTS AT 29D CEILING LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT 29D.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,208 hrs · 33,427 cycles
EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CABIN. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,208 hrs · 33,427 cycles
CEILING EMERGENCY LIGHTS AT 20D CEILING LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT 20D.
Earlier reports · 1995–2009 · 37 reports
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,184 hrs · 32,053 cycles
OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK.
Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 70,409 hrs
LGA - RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. RESEATED AFT BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 70,409 hrs
LGA - AFT STAIRWELL EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR AFT STAIRWELL EMERGENCY LIGHT.
Part: BATTERY PACK — NOT SEATED (EMERGENCY LIGHTS) · airframe 70,409 hrs
LGA - LEFT SIDE OVERWING EMERGENCY LIGHT INOPERATIVE. RESEATED AFT BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 70,409 hrs
LGA - AFT AISLE OVERHEAD EMERGENCY LIGHTS AT LAVATORY AREA INOPERATIVE. REPLACED BATTERY PACK AT AFT AISLE OVERHEAD.
Part: RELAY — INOPERATIVE (STAB TRIM) · airframe 70,383 hrs · 31,260 cycles
SFO - EMERGENCY DECLARED ON ACCOUNT OF FLIGHT CONTROL ISSUE-STABILIZER JAMMED UNABLE TO TRIM. RETURNED TO SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT PRIMARY AND ALT LONGITUDINAL TRIM SEEMED JAMMED IN FLIGHT. REPLACED PRIMARY STABILIZER TRIM RELAYS AND HORIZONTAL STABILIZER ACTUATOR CONTROL POWER UNIT SUPPLY. SYSTEM GROUND CHECK NORMAL OPERATION.
2008
Part: LIGHT — INOPERATIVE (CABIN) · 69,048 cycles
LGA EMERGENCY LIGHT AT EMERGENCY EXIT BULKHEAD INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT EMERGENCY EXIT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPS.
Part: REGULATOR — DEFECTIVE (CREW O2)
LAS INFLIGHT T1041/29JUL. CREW REPORTED CREW OXYGEN BOTTLE LOW. LANDED LAS WITHOUT INCIDENT. REPLACED CREW OXYGEN BOTTLE AND REGULATOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: B-NUT — LOOSE (OXYGEN SYSTEM) · airframe 67,487 hrs
IAD INFLIGHT T1281/17FEB BOS TO DFW - AT FL320 CREW REPORTED AIRCRAFT LOST PRESSURIZATION. OXYGEN MASKS DEPLOYED. LANDED IAD WITHOUT INCIDENT. SECURED LOOSE B NUT ON LEFT PACK SENSE LINE. FERRIED TO LGA. REPLACED ALL PASSENGER AND FLIGHT ATTENDANT OXYGEN CANISTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BATTERY PACK — DISCHARGED (CABIN)
LGA - EMERGENCY LIGHTS AT FORWARD OVERHEAD AISLE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD OVERHEAD AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN)
SFO - EMERGENCY LIGHT AT SEAT ROW 27 IS BROKEN. REPAIRED EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — DISCHARGED (CABIN)
LGA - EMERGENCY PATH LIGHTING AT ROW 20D TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY PATH LIGHTING AT ROW 20D TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — OVERHEATED (APU)
TUL - AUXILLARY POWER UNIT WIRE FEEDER CABLES, NUMBERS 3X2CAB, 3X2D2B, 3X1D2A AND 3X1C2A SHOWS SIGNS OF OVERHEATING. PLASTIC ADELON WIRE NUMBER 3X1C2A SHOWED SIGNS OF OVERHEATING. REPLACED AUXILLARY POWER UNIT WIRE FEEDER CABLES 3X2C2B, 3X2D2B, 3X1D2A, AND 3X1C2A AND ADEL CLAMP. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: TERMINAL — OVERHEATED (APU)
TUL - THREE WIRE RING TERMINALS SHOW SIGNS OF OVERHEATING AT RESISTER R4-9. REPLACED THREE EACH WIRE RING TERMINALS AT RESISTER R4-9. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND SKIN CRACKED AT CSK RIVET STATION 1380 JUST ABOVE RIGHT PYLON. STOP DRILLED CRACK, INSTALLED DOUBLER FS 1380 ON RIGHT SIDE PER AARD 53-30-00-02 PAGE 1 REV 8/30/02 AND SRM 53-01-00. (M)
Part: STRUCTURE — CRACKED (FUSELAGE)
TUL - FOUND WHALE BONE IS CRACKED AT FASTENER HOLE TOWARDS OUTBOARD END .5 INCH. INSTALLED DOUBLER PER AARD 53-10-00-12. (M)
2002
Part: LIGHT — INOPERATIVE (CABIN)
SEA - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERHEAD EMERGENCY EXIT LIGHT BY L2 FLIGHT ATTENDANT SEAT INOPERATIVE. TIGHTENED AFT OVERHEAD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SKIN — CRACKED (FUSELAGE)
TUL - FOUND FUSELAGE SKIN CRACKED AT STATION 1380 AND LONGERON 13L. INSTALLED DOUBLER PER SRM 51-01-00, 53-34-00 AND 53-30-00-2. (M)
2001
Part: ELEMENT — DEFECTIVE (TAIL)
DFW - FLT 2344 - DFW-MEX - AIR INTERRUPTED DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATION. RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT OVERHEAT ELEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WARNING LIGHT — FALSE INDICATION (COCKPIT)
DFW - EN ROUTE BNA-DFW - TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. TROUBLESHOT SYSTEM COULD NOT DUPLICATE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: ANGLE — CRACKED (FUSELAGE)
TUL - FOUND ANGLE CRACKED AT FASTENER, STATION 1474 CANT RIGHT SIDE, AT VERTICAL FIN ATTACHMENT. DAMAGE REMOVED FILLER AND DOUBLER INSTALLED PER AARD 53-10-00-2 AND ESO 80559 REF TO E58 3652093. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - FOUND CORROSION AROUND HOLE IN FORWARD END OF NR 6 SEAT TRACK WHERE GALLEY TIE DOWN ATTACHES. REPLACED SEAT TRACK STATION 218 TO 300 PER 53-05 FIG 4A. (M)
Part: WEB — CORRODED (FUSLEAGE)
TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 552, 541, 558, 560, AND 580 (INCORPORATES 3 E58 NOTED ON TOP). REMOVED FACTORY SECTION OF CUSP SHEET FROM STATION 503 TO STATION 598 AND INSTALLED A NEW SHEET (CUSP) PER SRM 51-01. (M)
Part: WEB — GOUGED (FUSELAGE)
TUL - FOUND LEFT CUSP, GOUGE IN RADIUS OF TEE STATION 737. REMOVED GOUGED AREA. INSTALLED REPAIR DOUBLER PER SRM SRM 53-05 FIG 25 PART 1 PAGE 60 E/E. (M)
Part: WEB — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON RIGHT CUSP AT STATION 620, 636 TO 655, 659 TO 662, AND 674 TO 693, WRITEUP INCORPORATE E58'S NOTED ABOVE). REMOVED FACTORY SECTION OF CUSP SHEET FROM STATION 598 TO 712 AND INSTALLED NEW CUSP SHEET PER SRM 51-01. (M)
Part: WEB — CORRODED (FUSELAGE)
TUL - FOUND RIGHT CUSP CORRODED STATION 1018 METAL SPLIT AT HOLE. INSTALLED DOUBLER WET PER AARD 53-00-00-02 AND SRM 53-01 PAGE 18 FIG 4 SHEET 3. (M)
Part: WEB — CORRODED (FUSLEAGE)
TUL - FOUND EXFOLIATED CORROSION TO CUSP STATION 1095-1098 RBL 57.5 - RBL 58.5, OUTBOARD OF SEAT TRACK NR 6. CUTOUT CORROSION, INSTALLED DOUBLER PER AARD 53-00-00-02. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - FOUND NR 1 SEAT TRACK CORRODED IN CHANNEL AND ON WORN LUG. REMOVED OUT OF LIMIT AREA OF NR 1 SEAT TRACK STATION 1234 TO 1237 AND INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4A (M)
Part: SEAT TRACK — WORN (FUSELAGE)
TUL - FOUND NR 4 SEAT TRACK WORN STATION 914-915. ACCOMPLISHED SEAT TRACK PLUG REPAIR PER AARD 53-20-00-10 REPAIR NR 10. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON NR 4 SEAT TRACK STATION 234. INSTALLED SEAT TRACK REPAIR PLUG PER SRM 53-04 FIG 4A. (M)
Part: LONGERON — CRACKED (FUSELAGE)
TUL - FOUND STATION 160 LONGERON 4 LEFT CRACKED IN RADIUS STATION 160 LONGERON 3 LEFT CRACKED IN RADIUS. REMOVED CRACKED SECTIONS OF LONGERON AND INSTALLED NEW LONGERONS AND SPLICES PER SRM 53-02 PAGES 48-53. (M)
Part: WIRE — SHORTED (GALLEY)
ORD - FLT 1694 - DURING FLIGHT, ELECTRICAL SPARKS REPORTED FROM TOP AFT GALLEY NUMBER 4 OVEN. CIRCUIT BREAKER POPPED AND SPARKS STOPPED. LEFT CIRCUIT BREAKER OPEN AND LANDED ORD WITHOUT INCIDENT. REPAIRED PINCHED WIRING HARNESS BETWEEN OVEN AND AIRCRAFT STRUCTURE. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED OVEN AS A PRECAUTION.. (M)
Part: LIGHT — INOPERATIVE (TAILCONE)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT TAILCONE RELEASE HANDLE LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT TAILCONE RELEASE HANDLE LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — BROKEN (AIR STAIR)
DFW - DURING OVERNIGHT MAINTENANCE SIDE WALL EMERGENCY EXIT LIGHT AT AFT STAIRWELL INOPERATIVE. REPLACED SIDE WALL EMERGENCY EXIT LIGHT AT AFT STAIRWELL. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: SUPPORT — DEFECTIVE (RT ENG FIRE DET)
MIA - FLT 1453 - EN ROUTE MIA-AUS - DURNIG CRUISE AT 35,000 FEET, RECEIVED A RIGHT ENGINE FIRE WARNING. ENGINE PARAMETERS APPEARED NORMAL. ACCOMPLISHED EMERGENCY PROCEDURES. BOTH FIRE BOTTLES WERE DISCHARGED. LIGHT EXTINGUISHED BRIEFLY, THEN CAME BACK ON FOR REMAINDER OF FLIGHT. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT ENGINE FIRE DETECTOR AMP AND ENGINE FIRE DETECTOR SUPPORT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL CONDUCTOR — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)